ES2236460T3 - Dispositivo de recuperacion de esfuerzos generados por un motor de aeronave. - Google Patents

Dispositivo de recuperacion de esfuerzos generados por un motor de aeronave.

Info

Publication number: ES2236460T3
Authority: ES; Spain
Prior art keywords: mast; reactor; fixed; fittings; engine
Prior art date: 2001-06-13
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Expired - Lifetime

Application number

ES02291443T

Other languages

English (en)

Spanish (es)

Inventor

Stephane Levert

Sebastien Roszak

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Airbus Operations SAS

Original Assignee

Airbus Operations SAS

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

2001-06-13

Filing date

2002-06-11

Publication date

2005-07-16

2002-06-11 Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS

2005-07-16 Application granted granted Critical

2005-07-16 Publication of ES2236460T3 publication Critical patent/ES2236460T3/es

2022-06-11 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Links

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Connection Of Plates (AREA)
Body Structure For Vehicles (AREA)
Clamps And Clips (AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Vibration Prevention Devices (AREA)
Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)

ES02291443T 2001-06-13 2002-06-11 Dispositivo de recuperacion de esfuerzos generados por un motor de aeronave. Expired - Lifetime ES2236460T3 (es)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
FR0107728		2001-06-13
FR0107728A FR2825976B1 (fr)	2001-06-13	2001-06-13	Dispositif de reprise d'efforts generes par un moteur d'aeronef

Publications (1)

Publication Number	Publication Date
ES2236460T3 true ES2236460T3 (es)	2005-07-16

Family

ID=8864260

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
ES02291443T Expired - Lifetime ES2236460T3 (es)	2001-06-13	2002-06-11	Dispositivo de recuperacion de esfuerzos generados por un motor de aeronave.

Country Status (7)

Country	Link
US (1)	US6648271B2 (de)
EP (1)	EP1266826B1 (de)
AT (1)	ATE288384T1 (de)
CA (1)	CA2389881C (de)
DE (1)	DE60202813T2 (de)
ES (1)	ES2236460T3 (de)
FR (1)	FR2825976B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2887851B1 (fr) *	2005-06-29	2007-08-17	Airbus France Sas	Mat d'accrochage de moteur pour aeronef
FR2891248B1 (fr) *	2005-09-28	2009-05-01	Airbus France Sas	Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891249B1 (fr) *	2005-09-28	2009-05-01	Airbus France Sas	Mat d'accrochage de moteur pour aeronef
FR2891255B1 (fr) *	2006-07-07	2007-10-26	Airbus France Sas	Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2915176B1 (fr) *	2007-04-20	2009-07-10	Airbus France Sa	Mat d'accrochage de moteur pour aeronef disposant d'une attache moteur arriere pourvue d'un ecrou a barillet
FR2926788B1 (fr) *	2008-01-25	2010-04-02	Snecma	Fixation d'un turboreacteur multiflux a un aeronef
FR2929245B1 (fr) *	2008-03-28	2010-05-14	Aircelle Sa	Structure primaire d'un mat d'accrochage.
GB0810589D0 (en) *	2008-06-11	2008-07-16	Rolls Royce Plc	Engine mounting arrangement
JP6266775B2 (ja)	2013-07-26	2018-01-24	エムアールエイ・システムズ・エルエルシー	航空機エンジンパイロン
GB201315968D0 (en) *	2013-09-09	2013-10-23	Rolls Royce Plc	Aircraft engine mount
FR3059982B1 (fr) *	2016-12-14	2022-07-29	Airbus Operations Sas	Ensemble support pour un moteur d'aeronef

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2291091A1 (fr) *	1974-11-13	1976-06-11	Snecma	Dispositif de montage sur avion d'un turboreacteur
GB2061389B (en) *	1979-10-23	1983-05-18	Rolls Royce	Rod installation for a gas turbine engine
US4725019A (en) *	1986-08-11	1988-02-16	The Boeing Company	Aircraft engine mount with vertical vibration isolation
FR2622930B1 (fr) *	1987-11-06	1990-03-23	Aerospatiale	Capotage pour turboreacteur a double flux
US5275357A (en)	1992-01-16	1994-01-04	General Electric Company	Aircraft engine mount
US5443229A (en) *	1993-12-13	1995-08-22	General Electric Company	Aircraft gas turbine engine sideways mount
US5620154A (en)	1995-05-03	1997-04-15	The Boeing Company	Three link failsafe engine mount
US5927644A (en) *	1997-10-08	1999-07-27	General Electric Company	Double failsafe engine mount
US5921500A (en) *	1997-10-08	1999-07-13	General Electric Company	Integrated failsafe engine mount
FR2770486B1 (fr)	1997-11-06	2000-01-28	Aerospatiale	Dispositif d'accrochage d'un moteur sur un aeronef
US6189830B1 (en) *	1999-02-26	2001-02-20	The Boeing Company	Tuned engine mounting system for jet aircraft
GB9927425D0 (en) *	1999-11-20	2000-01-19	Rolls Royce Plc	A gas turbine engine mounting arrangement

2001
- 2001-06-13 FR FR0107728A patent/FR2825976B1/fr not_active Expired - Fee Related
2002
- 2002-06-07 US US10/165,563 patent/US6648271B2/en not_active Expired - Lifetime
- 2002-06-10 CA CA2389881A patent/CA2389881C/en not_active Expired - Fee Related
- 2002-06-11 ES ES02291443T patent/ES2236460T3/es not_active Expired - Lifetime
- 2002-06-11 AT AT02291443T patent/ATE288384T1/de not_active IP Right Cessation
- 2002-06-11 DE DE60202813T patent/DE60202813T2/de not_active Expired - Lifetime
- 2002-06-11 EP EP02291443A patent/EP1266826B1/de not_active Expired - Lifetime

Also Published As

Publication number	Publication date
DE60202813T2 (de)	2006-05-04
EP1266826B1 (de)	2005-02-02
FR2825976A1 (fr)	2002-12-20
ATE288384T1 (de)	2005-02-15
CA2389881A1 (en)	2002-12-13
FR2825976B1 (fr)	2003-09-05
US20030173456A1 (en)	2003-09-18
CA2389881C (en)	2010-04-27
DE60202813D1 (de)	2005-03-10
US6648271B2 (en)	2003-11-18
EP1266826A1 (de)	2002-12-18

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